REPUBLIC OF SERBIA

MINISTRY OF DEFENCE

www.mod.gov.rs

MINISTRY OF DEFENCE

Material Resources Sector

Defensive Technologies Department

Military Technical Institute

www.vti.mod.gov.rs

test simulator for the discrete multi-parametric decision flight system

Stojan MarkoviĆ

University of defense, Military academy, Belgrade, Serbia, stomarkovic@yahoo.com

MomČilo MilinoviĆ

Faculty of Mechanical Engineering, University of Belgrade, Sertbia, mmilinovic@mas.bg.ac.rs

NENAD SAKAN

Institute of Physics, University of Belgrade, Serbia, nsakan@ipb.ac.rs

Abstract: The system concept, decision making mathematical model and top level algorithm for multi-parametric singular system for the missile control and guidance is presented. As a part of the research, a software top level algorithm is yielded and experimentally tested and proven by the means of the hardware test system. The systems runs multi-parametric criteria decision functionality simultaneously and sequentially, on each of the flight and ground based objects, coupled by singular decision functions. The studied system present the set of controlled objects interconnected in the system capable of adopting to the external stimuli as well as internal conditions changes. Such simulation hardware serves as operational test of concept for the mentioned adoptable system of controlled coupled objects, interconnected in the decision making process in the simulation of real flight conditions as an add-on hardware to the real missile. The studied mathematical relations that provided model for the decision making process in the operational algorithms are visualized in the experiments, and a set of parameters of the well behaved model is presented.

Keywords: missile guidance, control system synthesis, decentralized control, decision making, singular system.